What was found
THE AIRCRAFT JACKING PROCESS, THE UPPER FUSELAGE AT CROWN AREA WAS TOUCHED BY ADJACENT SCAFFOLDING, AND CAUSED DAMAGES AT TWO SEPARATED AREAS AS FOLLOWS: DAMAGE LOCATION 1– DENT #1 LOCATED AT STA 500C+20.5” AND BETWEEN STR 8RH AND STR 9RH. DAMAGE LOCATION 2- DENT #2 WITH GOUGE LOCATED BETWEEN STA 480 AND STA 500 AND BETWEEN STR-8RH AND STR-10RH. ACCOMPLISHED THE SKIN DENT -1 REPAIR "LEFT AS IS" AS PER COOPESA ENGINEERING ORDER # COO-EO-2024-19643-R00, DATED MARCH 12, 2024, BOEING REPAIR INSTRUCTIONS "LEAVE AS IS" AND FINAL APPROVAL PER RDR DOCUMENT PROVIDED BY BOEING. ACCOMPLISHED THE SKIN DENT -2 REPAIR "SKIN CUT OUT" AS PER COOPESA ENGINEERING ORDER # COO-EO-2024-19642-R00, DATED MARCH 12, 2024, BOEING REPAIR INSTRUCTIONS "SKIN CUT OUT" AND FINAL APPROVAL PER FAA FORM 8100-9 PROVIDED BY BOEING.